GB2186084A - Determination of the spectral content of transient stress wave events - Google Patents
Determination of the spectral content of transient stress wave events Download PDFInfo
- Publication number
- GB2186084A GB2186084A GB08602823A GB8602823A GB2186084A GB 2186084 A GB2186084 A GB 2186084A GB 08602823 A GB08602823 A GB 08602823A GB 8602823 A GB8602823 A GB 8602823A GB 2186084 A GB2186084 A GB 2186084A
- Authority
- GB
- United Kingdom
- Prior art keywords
- stress wave
- transducer
- spectral content
- transient stress
- wave event
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000001052 transient effect Effects 0.000 title claims description 49
- 230000003595 spectral effect Effects 0.000 title claims description 32
- 235000019687 Lamb Nutrition 0.000 claims description 21
- 238000000034 method Methods 0.000 claims description 16
- 238000006073 displacement reaction Methods 0.000 claims description 14
- 238000004458 analytical method Methods 0.000 claims description 5
- 230000001143 conditioned effect Effects 0.000 claims description 2
- 230000003750 conditioning effect Effects 0.000 claims description 2
- 239000000306 component Substances 0.000 claims 1
- 238000009795 derivation Methods 0.000 claims 1
- 238000005070 sampling Methods 0.000 claims 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 238000012512 characterization method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 101100400378 Mus musculus Marveld2 gene Proteins 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910001235 nimonic Inorganic materials 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
- G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
- G01H1/04—Measuring characteristics of vibrations in solids by using direct conduction to the detector of vibrations which are transverse to direction of propagation
- G01H1/06—Frequency
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R23/00—Arrangements for measuring frequencies; Arrangements for analysing frequency spectra
- G01R23/16—Spectrum analysis; Fourier analysis
- G01R23/17—Spectrum analysis; Fourier analysis with optical or acoustical auxiliary devices
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mathematical Physics (AREA)
- Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Description
1 GB2186084A 1
SPECIFICATION
Determination of the spectral content of transient stress wave events 5 This invention relates to the determination of the spectral content of transient stress wave 5 events in plate-like structures.
It is frequently desirable to determine the spectral content of transient stress wave events. Analysis of the resultant spectral content may be utilised, for instance, in the calibration of broad frequency band acoustic emission transducers and the characterisation of impacts upon 10 structures. Impact characterisation can be very useful in sorting applications in which a number 10 of articles sequentially impacting a given surface are to be sorted between like and unlike articles. The spectral content of transient stress events involving the like articles are similar and not the same as the spectral content- of transient stress wave events involving the unlike articles.
15 Spectral content determination of transient stress wave events can be achieved with the use 15 of a transient recorder and computational (Fourier Transform) analysis. However this tends to be complicated and expensive.
It is an object of the present invention to provide a method of and apparatus for the spectral content determination of transient stress wave events in plate-like structures which is character 20 ised both by greater simplicity and cheapness than has heretofore been achieved. 20 According to the present invention, a method of determining at least a portion of the spectral content of a transient stress wave event occuring on one surface of a plate-like structure having opposed surfaces comprises locating a transducer on one of said surfaces which transducer is responsive to and has an output representative of any displacement of said surface upon which 25 it is mounted, causing a transient stress wave event to take place on one of said surfaces at a 25 position remote from said transducer so that Lamb waves resulting from and characteristic of said stress wave event propogate through said plate-like structure in a dispersive manner to cause correspondingly characteristic displacement of said surfaces including that portion of the surface upon which said transducer is mounted, analysing the output of said transducer to 30 determine the characteristics of said Lamb waves and deriving therefrom at least a portion of 30 the spectral content of said transient stress wave event.
According to a further aspect of the present invention, apparatus suitable for the determination of at least a portion of the spectral content of a transient stress wave event comprises a platelike structure having opposed surfaces, a transducer located on one of those opposed surfaces 35 which transducer is responsive to and has an output representative of any displacement of the 35 surface upon which it is mounted, and signal processing means adapted to monitor and process the output of said transducer, said plate-like structure being so disposed as to be subject to the occurence of a transient stress-wave event on one of said surfaces thereof at a position remote from said transducer so that Lamb waves resulting from and characteristic of any such stress wave event propogate through said plate-like structure in a dispersive manner to cause corre4C spondingly characteristic displacement of said surfaces including that portion of the surface upon which said transducer is mounted, said signal processing means being adapted to monitor and process the output of said transducer in such a manner as to provide an indication of those characteristics of said Lamb waves from which at least a portion of the spectral content of any 45 such stress wave event may be derived. 4 The invention will now be described, by way of example, with reference to the accompanying drawings in which Figure 1 is a graph indicating the dependence of Lamb wave group velocity on frequency and plate thickness.
50 Figure 2 is a diagrammatic representation of apparatus in accordance with the present inven- 50 tion.
Figure 3 is a graph indicating the detected surface displacement of a plate surface at a distance of 9Omm from a transient stress wave event.
Figure 4 is an indicatjion of the spectral content of the transient stress wave event causing the 55 surface displacement indicated in Fig. 3. 55 If a plate-like structure is subject to a transient stress wave event on one of its surfaces, for instance impact by an object, resultant stress waves propogate through that structure as Lamb waves. Lamb waves (or plate waves as they are sometimes referred to) are characterised by wave activity across the opposed surfaces of the plate-like structure. The wave activity across 60 the opposed surfaces is interelated so that the waves are either in or out of phase with each 60 other. These are referred to as being antisymmetric or symmetric. Moreover a family of symme tric and antisymmetric Lamb wave modes is possible following a transient stress wave event as can be seen from Fig. 1. Fig. 1 illustrates the dependence of Lamb wave group velocity within a plate-like structure on frequency and plate thickness, those waves designated So to S2 being 65 symmetric and those designated a. to a2 being antisymmetric. Fig. 1 also illustrates a further 65 -2 GB2186084A 2 important property of Lamb waves viz. that they are dispersive.Thus the velocity of propogation of Lamb waves is dependent upon wave frequency.
It is the dispersive nature of Lamb waves which is utilised in the method and apparatus of the present invention. Thus the present invention relies upon the dispersion of Lamb waves to 5 separate the various frequency components which are contained in a localised transient stress 5 wave.
Referring to Fig. 2, the apparatus of the present invention is generally indicated at 10. The apparatus 10 comprises a plate 11 formed from the nickel base alloy known as Nimonic 75 having a piezo-electric transducer 12 attached to its upper surface. The piezo-electric transducer 12 is responsive to a broad band of frequencies and is adapted to provide an electrical output 10 which is characteristic of any displacement of the surface of the plate 11 to a charge amplifier 13. The output of the charge amplifier 13 is fed to an envelope follower 14, the output of which is fed An turn to a logarithmic amplifier 15. The logarithmic amplifier 15 output is directed to a sample and hold device 16 and thence to an appropriate display device 17, the output of 15 the sample and hold device 16 being controlled by a pulse generator 18, 15 The apparatus 10 is used in the determination of the spectral content of a localised transient stress wave event occuring on the same surface of the plate 11 as the transducer 12 but originating at a position 19 which is remote from the transducer 12. The particular transient event chosen to investigate the characteristics of the present invention was the breaking of a 20 pencil lead on the plate 11 at the position 19. It will be appreciated however other transient 20 events such as impacts, step release functions or rapid localised thermal expansion could be utilised if so desired. Moreover it will be appreciated that since Lamb waves result in character istic displacement of both the upper and lower faces of the plate 11, the transducer could be positioned on the lower face if so desired.
25 In order to simplify the interpretation of the waveforms resulting from the localised transient 25 stress wave event at 19, we prefer to arrange for the propogation of the waves to be predominantly in only one of the Lamb modes and for the group velocity not to pass through a maxima or minima. This can be achieved by ensuring that the plate 11 is of a constant thickness which is selected so that the following expression is satisfied:
30 30 d<C 2nf where 35 d=plate half thickness C=shear wave velocity f=maximum frequency in the bandwidth of interest.
Under these conditions, the lowest order antisymmetric mode (a.) predominates and the velocity of propagation increases in a non-linear manner with frequency. Thus when the localised 40 transient stress wave event is generated by the breaking of the pencil lead at the position 19, the various frequency components associated with that event become physically separated across the plate 11 as they propogate as Lamb waves. The resultant surface displacement detected by the transducer 12 results in it providing an electrical output characteristic of that displacement and hence the frequency components of the transient stress wave event as can be 45 seen from Fig. 3. i A simple analysis of the amplitudes and periods of the oscillations in the waveform shown in Fig. 3 was used to arrive at the spectrum shown in Fig. 4. The amplitude scale of Fig. 4 is logarithmic and it will be noted that the approximately linear negative slope at 20d13/decade of 50 the spectrum indicates a l/f dependence. This confirms the method of the present invention as 50 an effective method of spectral content determination since it is well known that a step function (such as a pencil lead break) has a spectral content with a l/frequency dependence.
The above analysis of the output of the transducer 12 is relatively crude and it is therefore desirable to provide a more effective means for processing the output. This is achieved by 55 suitable conditioning of the transducer 12 output signal by the charge amplifier 13, envelope 55 follower 14 and logarithmic amplifier 15. The conditioned signal is then passed to the sample and hold device 16 the output of which is, as previously stated, controlled by the pulse generator 18. The operation of the pulse generator 18 is initiated by a signal via line 19 from an appropriate detector (not shown) positioned adjacent the source of the transient stress wave 60 event upon the occurence of the transient stress wave event. The pulse generator then causes 60 the sample and hold device 16 to pass a signal to the display device 17 at discrete time periods corresponding with the passage of frequency components of the transient stress wave event pssing the transducer 12. Thus as previously stated the various frequency components of the transient stress wave event propogate as Lamb waves through the plate 11 at different 65 rates. Consequently the frequency component of the waveform which is intercepted by the 65 GB2186084A 3 transducer 12 at any point is determined from the total propogation time since this can be related to frequency using the theoretical solution as plotted in Fig. 1 and making use of the relationship velocity= distance/time.
The display provided by the device 17 can therefore be of the total spectral content of the 5 transient stress wave event if so desired. This could be useful in the calibration of arl unknown 5 transducer 12 using a known transient stress wave event.
It may be desirable in other circumstances however to sample only parts of the spectral content of a transient stress wave event which are known to be characteristic of that event.
This could be useful, for instance, in the sorting of components. A succession of components 10 would be dropped under identical conditions on to the same location on the plate 11. If any of 10 those components were to be, for instance, of different hardness to the remainder, it would cause a transient stress wave event having a different spectral content to that characteristic of the remainder of the components. It will be appreciated however that other different component characteristics could be utilised if so desired. For instance mention may be made of Youngs 15 Modulus, Poissons ratio, radius at the point of impact, velocity and mass. This would be 15 highlighted by the display on the device 17, thereby giving an indication of the presence of a non-standard component.
It will be seen therefore that the method and apparatus of the present invention provide a simple and cheap means for deriving the spectral content of a transient stress wave event.
20 20
Claims (7)
1. A method of determining at least a portion of the spectral content of a transient stress wave event occuring on one surface of a plate-like structure having opposed surfaces comprising locating a transducer on one of said surfaces which transducer is responsive to and has an 25 output representative of any displacement of said surface upon which it is mounted, causing a 25 transient stress wave event to take place on one of said surfaces at a position remote from said transducer so that Lamb waves resulting from and characteristic of said transient stress wave event propogate through said plate like structure in a dispersive manner to cause correspondin gly characteristic displacement of said surfaces including that portion of the surface upon which 30 said transducer is mounted, analysing the output of said transducer to determine the character- 30 istics of said Lamb waves and deriving therefrom at least a portion of the spectral content of said transient stress wave event.
2. A method of determining at least a portion of the spectral content of a transient stress wave event as claimed in claim 1 wherein said opposed surfaces of said plate-like structure are 35 parallel. 35
3. A method of determining at least a portion of the spectral content of a transient stress wave. event as claimed in claim 2 wherein d<C 40 -
4.0 2 7rf where d=plate half thickness 45 C=shear wave velocity 4E f=maximum frequency in the bandwidth of interest 4. A method of determining at least a portion of the spectral content of a transient stress wave event as claimed in any one preceding claim wherein the analysis of the output of said transducer and the derivation of said at least a portion of the spectral content of said transient 50 stress wave event comprises appropriately conditioning said transducer output and subsequently 5.' sampling and displaying said output at discrete time intervals from the occurence of said transient stress wave event in accordance with the rate of propogation of the frequency compo nents of said transient stress wave event through said plate-like structure.
5. A method of determining at least a portion of the spectral content of a transient stress 55 wave event as claimed in claim 4 wherein said transducer output is appropriately conditioned by 55 a charge amplifier, an envelope follower and a logarithmic amplifier.
6. Apparatus suitable for the determination of at least a portion of the spectral content of a transient stress wave event comprising a plate-like structure having opposed surfaces, a trans ducer located on one of the opposed surfaces which transducer is responsive to and has an 60 output representative of any displacement of the surface upon which it is mounted, and signal 60 processing means adapted to monitor and process the output of said transducer, said plate-like structure being so disposed as to be subject to the occurence of a transient stress wave event on one of the surfaces thereof at a position remote from said transducer so that Lamb waves resulting from and characteristic of any such stress wave event propogate through said plate-like 65 structure in a dispersive manner to cause correspondingly characteristic displacement of said 65 4 GB2186084A 4 surfaces including that portion of the surface upon which said transducer is mounted, said signal processing means being adapted to monitor and process the output of said transducer in such a manner as to provide an indication of those characteristics of said Lamb waves from which at least a portion of the spectral content of any such stress wave event may be derived.
5
7. A method of determining the spectral content of a transient stress wave event substan- 5 tially as hereinbefore described with reference to the accompanying drawings.
8, Appararatus suitable for the determination of at least a portion of the spectral content of a transient stress wave event substantially as hereinbefore described with reference to the accompanying drawings.
Printed for Her Majesty's Stationery Office by Burgess & Son (Abingdon) Ltd, Dd 8991685, 1987. Published at The Patent Office, 25 Southampton Buildings, London, WC2A 1 AY, from which copies may be obtained.
i k
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB858509836A GB8509836D0 (en) | 1985-04-17 | 1985-04-17 | Transient stress wave events |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8602823D0 GB8602823D0 (en) | 1986-03-12 |
| GB2186084A true GB2186084A (en) | 1987-08-05 |
| GB2186084B GB2186084B (en) | 1989-05-24 |
Family
ID=10577791
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB858509836A Pending GB8509836D0 (en) | 1985-04-17 | 1985-04-17 | Transient stress wave events |
| GB8602823A Expired GB2186084B (en) | 1985-04-17 | 1986-02-05 | Determination of the spectral content of transient stress wave events |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB858509836A Pending GB8509836D0 (en) | 1985-04-17 | 1985-04-17 | Transient stress wave events |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4688429A (en) |
| JP (1) | JPS61270638A (en) |
| DE (1) | DE3611967A1 (en) |
| FR (1) | FR2580816B1 (en) |
| GB (2) | GB8509836D0 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2275845A (en) * | 1993-03-05 | 1994-09-07 | Bae Sema Ltd | Sonar transducers |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5035144A (en) * | 1989-07-31 | 1991-07-30 | National Research Council Of Canada | Frequency broadband measurement of the characteristics of acoustic waves |
| US5532538A (en) * | 1994-10-28 | 1996-07-02 | Jin; Yu | Sensing and signal processing devices using quasi-SH (shear horizontal) acoustic waves |
| US5635643A (en) * | 1995-03-15 | 1997-06-03 | The University Of New Mexico | Identifying source of acoustic emissions in structures using lamb waves and vibration modes |
| US6715354B2 (en) | 1998-02-24 | 2004-04-06 | Massachusetts Institute Of Technology | Flaw detection system using acoustic doppler effect |
| US6253618B1 (en) | 1999-12-08 | 2001-07-03 | Massachusetts Intitute Of Technology | Apparatus and method for synthetic phase tuning of acoustic guided waves |
| US6728515B1 (en) | 2000-02-16 | 2004-04-27 | Massachusetts Institute Of Technology | Tuned wave phased array |
| US6360609B1 (en) * | 2000-02-23 | 2002-03-26 | Massachusetts Institute Of Technology | Method and system for interpreting and utilizing multimode dispersive acoustic guided waves |
| US6575036B1 (en) * | 2000-06-22 | 2003-06-10 | The Boeing Company | Method for in-situ nondestructive measurement of Young's modulus of plate structures |
| US6920790B2 (en) * | 2000-06-22 | 2005-07-26 | The Boeing Company | Apparatus for in-situ nondestructive measurement of Young's modulus of plate structures |
| US6833554B2 (en) * | 2000-11-21 | 2004-12-21 | Massachusetts Institute Of Technology | Laser-induced defect detection system and method |
| RU2540942C1 (en) * | 2013-11-07 | 2015-02-10 | Общество с ограниченной ответственностью "ИНТЕРЮНИС" | Method to monitor dynamics of variation of controlled object wall thickness |
| JP6329188B2 (en) * | 2016-02-29 | 2018-05-23 | 株式会社Subaru | Ultrasonic inspection system, ultrasonic inspection method and aircraft structure |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1198621A (en) * | 1966-05-06 | 1970-07-15 | Donald Orr Sproule | The Correction of the Undesirable Effects of Dispersion on Signals. |
| GB1545505A (en) * | 1975-09-16 | 1979-05-10 | Ca Minister Nat Defence | Excitation and spectral calibration of acoustic emission systems |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3572099A (en) * | 1968-08-23 | 1971-03-23 | Gen Am Transport | Ultrasonic non-destructive testing apparatus and method |
| FR2049304A5 (en) * | 1969-06-06 | 1971-03-26 | Realisations Ultrasoniques Sa | |
| DE2632323C3 (en) * | 1976-07-17 | 1979-02-22 | Thyssen Niederrhein Ag Huetten- Und Walzwerke, 4200 Oberhausen | Device for ultrasonic testing of plate-shaped bodies, in particular sheet metal strip, using the pulse-echo method with Lamb waves |
| US4218924A (en) * | 1979-07-02 | 1980-08-26 | Rockwell International Corporation | Ultrasonic ellipsometer |
| GB8402098D0 (en) * | 1984-01-26 | 1984-02-29 | Atomic Energy Authority Uk | Ultrasonic inspection of tube |
-
1985
- 1985-04-17 GB GB858509836A patent/GB8509836D0/en active Pending
-
1986
- 1986-02-05 GB GB8602823A patent/GB2186084B/en not_active Expired
- 1986-03-06 US US06/837,031 patent/US4688429A/en not_active Expired - Fee Related
- 1986-04-09 DE DE19863611967 patent/DE3611967A1/en not_active Withdrawn
- 1986-04-14 FR FR868605264A patent/FR2580816B1/en not_active Expired
- 1986-04-17 JP JP61089159A patent/JPS61270638A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1198621A (en) * | 1966-05-06 | 1970-07-15 | Donald Orr Sproule | The Correction of the Undesirable Effects of Dispersion on Signals. |
| GB1545505A (en) * | 1975-09-16 | 1979-05-10 | Ca Minister Nat Defence | Excitation and spectral calibration of acoustic emission systems |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2275845A (en) * | 1993-03-05 | 1994-09-07 | Bae Sema Ltd | Sonar transducers |
| GB2275845B (en) * | 1993-03-05 | 1997-04-23 | Bae Sema Ltd | Sonar transducers |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2580816A1 (en) | 1986-10-24 |
| GB2186084B (en) | 1989-05-24 |
| DE3611967A1 (en) | 1986-10-30 |
| GB8602823D0 (en) | 1986-03-12 |
| JPS61270638A (en) | 1986-11-29 |
| FR2580816B1 (en) | 1989-08-25 |
| US4688429A (en) | 1987-08-25 |
| GB8509836D0 (en) | 1985-05-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19940205 |